|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-027/04 B64C-021/06 B64D-033/02|
|미국특허분류(USC)||244/017.11; 244/053B; 244/209|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 3|
A helicopter comprising a drive having an air intake conduit, a main rotor connected functionally to the drive and a transmission interposed functionally between the main rotor and the drive and housed in a housing. The helicopter further comprises at least one air intake having a first inlet fluidly connected to the intake conduit, at least one second inlet fluidly connected to the housing and deflecting means interacting, in use, with an airflow to divide the airflow into a first and a second airflow. The air intake also has guide means for guiding the...
1. A helicopter (1) comprising: a fuselage (2);a drive (6) comprising an air intake conduit (12);a main rotor (3) connected functionally to said drive (6);a transmission (9) interposed functionally between said main rotor (3) and said drive (6) and housed in a housing (23); andat least one air intake (20) comprising: a first inlet (21) fluidly connected to said intake conduit (12);at least one second inlet (22) fluidly connected to said housing (23);a first wall (29) defining deflecting means (30) interacting, in use, with an airflow (F) to divide the ai...